Author Topic: SpaceX Falcon 9 FT - ORBCOMM-2 - Dec. 21, 2015 (Return To Flight) DISCUSSION  (Read 1360669 times)

Offline philw1776

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FULL SEND!!!!

Offline ugordan

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Try this site for all F9 launches

http://www.flightclub.io/results.php?id=f6a20bfa-2802-480d-b66f-282aba6a7efe&code=OG22

That is impressive, but as far as I can see those are just simulations, not actual data. Unless SES-9 and Jason-3 already launched.

edit: added trajectory plot with 1 minute tick marks:
« Last Edit: 12/30/2015 06:49 pm by ugordan »

Online Steven Pietrobon

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That's great work ugordan! Would it be possible to obtain an inertial speed versus time plot?
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline Roy_H

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That's great work ugordan! Would it be possible to obtain an inertial speed versus time plot?

Excuse my ignorance, but he already has a speed vs time plot. What is the difference for "inertial" speed. And please add a definition. Thanks.
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Offline baldusi

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That's great work ugordan! Would it be possible to obtain an inertial speed versus time plot?

Excuse my ignorance, but he already has a speed vs time plot. What is the difference for "inertial" speed. And please add a definition. Thanks.
Inertial speed means discounting the rotation of the Earth.

Offline cscott

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I assume that's what's been already been plotted, since the graphs start at speed=0.

EDIT: ah, when you said "discounting" you really meant "accounting for and including".
« Last Edit: 12/31/2015 07:56 pm by cscott »

Offline baldusi

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If it was inertial it would have started at some 350m/s or so from the rotation of the Earth at the Cape.

Offline Arb

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A day before launch and some days after LRR Elon delayed the flight by 24 hours for a 10% improvement in the chance of landing success. This led to some discussion. A later thread on SpaceX Systems Engineering contains a relevant slide showing FRR as a continuous process from WDR to Launch.

The slide also suggests that WDR and static fires will always be part of their process.

Interesting stuff.

Edit: Clarification
« Last Edit: 12/31/2015 07:50 pm by Arb »

Offline Kabloona

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Quote
The slide also suggests that WDR and static fires will always be part of their process.

I'd be careful about saying "always." That slide was from 2012, and since then they've combined WDR into the static fire, so there aren't going to be any more standalone WDR's.

Offline Arb

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Quote
The slide also suggests that WDR and static fires will always be part of their process.
I'd be careful about saying "always." That slide was from 2012, and since then they've combined WDR into the static fire, so there aren't going to be any more standalone WDR's.


And if they achieve their long-term goal of:
Quote from:  SpaceX Tooling Manager (Travel Team) job advert - http://www.spacex.com/careers/position/7829
[a] fully automated launch system capable of rolling the vehicle to the pad, raising it to position, fueling, and executing a full launch sequence in a single hour
then there likely won't be time for a static fire. But for now they still do both, albeit combined.


Edit: Quote formatting.
« Last Edit: 12/31/2015 10:01 pm by Arb »

Offline AJW

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Is it your gamma boost, or did somebody get a bath?
We are all interested in the future, for that is where you and I are going to spend the rest of our lives.

Offline oiorionsbelt

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Screen shot of the Instagram picture
« Last Edit: 12/31/2015 11:48 pm by oiorionsbelt »

Offline docmordrid

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Only boosted it a small amount for the shadows. Looks like it's had a wash.
« Last Edit: 12/31/2015 11:50 pm by docmordrid »
DM

Offline Jdeshetler

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After looking at Elon's photo of "used" F9 where there is lots of chipped and bubbled painted surfaces which is only superficial. 

The Space Shuttle saved 600 lbs after stopping painting the white latex paint on the 3rd exterior tank. So why not no more white paint on F9 and it might save 200 to 300 lbs plus no more chipped paints to check out for loose flakes....

Offline pathfinder_01

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After looking at Elon's photo of "used" F9 where there is lots of chipped and bubbled painted surfaces which is only superficial. 

The Space Shuttle saved 600 lbs after stopping painting the white latex paint on the 3rd exterior tank. So why not no more white paint on F9 and it might save 200 to 300 lbs plus no more chipped paints to check out for loose flakes....

The white paint on the Shuttle was to help keeping the tank at the proper temperature. It was simply discovered that it was not needed and removing it improved performance and saved money. Likewise Elon might have to evaluate that first.

Offline sdsds

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You might ask, "Why do the static fire test?" I think the answer is that otherwise much may have happened since you last saw the engines' shutdown transient behavior.
— 𝐬𝐝𝐒𝐝𝐬 —

Offline NovaSilisko

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I don't think Musk would ever go for an unpainted Falcon 9. He refused to let Grasshopper be shown until it was painted and given the SpaceX logo, IIRC - whereas the engineers were just going to fly it "naked".

Offline Jdeshetler

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Anodized the aluminum surface is one way of adding color and some protection however white is the only color can't be applied thru this procedure.....

Offline rcoppola

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What are these cracks/peels on the grid fins?
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Offline Kabloona

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What are these cracks/peels on the grid fins?

Probably a thin layer of thermal protection (SPAM?) that peeled off.

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